FIELD: proposed control systems is used in an emergency in case of failure of electric control system. SUBSTANCE: proposed fluidic control system includes sensors showing position of control sticks and parameters of motion of flying vehicle and pneumofluidic computer connected with hydraulic actuator. Sensors and computer are connected by means of hydraulic lines including air-liquid and liquid-air media dividers which are provided with fluidic amplifiers. EFFECT: avoidance of transit lag of control signals stipulated by compressibility of gaseous medium. 1 dwg
